Difference between revisions of "User:DnaGonite/Tornado GR.1"
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Revision as of 20:58, 10 February 2023
| This page is about the British strike aircraft U38088265/Tornado GR.1. For other versions, see Tornado (Family). |
Contents
Description
The Tornado GR.1 is a rank VIII British strike aircraft with a battle rating of 11.7 (AB/RB/SB). It was introduced in Update "Apex Predators".
General info
Flight performance
Max speed
at 10 972 m2 005 km/h
Turn time31 s
Max altitude12 800 m
EngineTurbo-Union RB199-34R Mk.101
Type
Cooling systemAir
Describe how the aircraft behaves in the air. Speed, manoeuvrability, acceleration and allowable loads - these are the most important characteristics of the vehicle.
| Characteristics | Max speed (km/h at 10,972 m) |
Max altitude (metres) |
Turn time (seconds) |
Rate of climb (metres/second) |
Take-off run (metres) | |||
|---|---|---|---|---|---|---|---|---|
| AB | RB | AB | RB | AB | RB | |||
| Stock | 1,991 | 1,991 | 12800 | 31.4 | 31.5 | 155.1 | 152.8 | 800 |
| Upgraded | ___ | ___ | __._ | __._ | __._ | __._ | ||
Details
| Features | |||||
|---|---|---|---|---|---|
| Combat flaps | Take-off flaps | Landing flaps | Air brakes | Arrestor gear | Drogue chute |
| ✓ | ✓ | ✓ | ✓ | ✓ | X |
| Limits | Wings (km/h) | Gear (km/h) | Flaps (km/h) | Max Static G | |||
|---|---|---|---|---|---|---|---|
| Combat | Take-off | Landing | + | - | |||
| Min sweep | 972 | 0 | 1,166 | 552 | 440 | ~8 | ~3 |
| Max sweep | 1,555 | ~9 | ~3 | ||||
| Optimal velocities (km/h) | |||
|---|---|---|---|
| Ailerons | Rudder | Elevators | Radiator |
| < 670 | < 650 | < 700 | N/A |
Engine performance
| Engine | Aircraft mass | ||||||||
|---|---|---|---|---|---|---|---|---|---|
| Engine name | Number | Basic mass | Wing loading (full internal fuel) | ||||||
| Turbo-Union RB199-34R Mk.101 | 2 | 14,309 kg | 634 kg/m2 | ||||||
| Engine characteristics | Mass with internal fuel (no weapons load or external fuel) | Max Takeoff Weight | |||||||
| Weight (each) | Type | 17m fuel | 20m fuel | 30m fuel | 45m fuel | 58m fuel | |||
| 2,200 kg | Afterburning low-bypass turbofan | 15,801 kg | 16,064 kg | 16,942 kg | 18,258 kg | 19,399 kg | 27,200 kg | ||
| Maximum engine thrust @ 0 m (RB/SB) | Thrust to weight ratio @ 0 m (WEP) | ||||||||
| Condition | 100% | WEP | 17m fuel | 20m fuel | 30m fuel | 45m fuel | 58m fuel | MTOW | |
| Stationary | 3,633 kgf | 7,015 kgf | 0.89 | 0.87 | 0.83 | 0.77 | 0.72 | 0.52 | |
| Optimal | 4,032 kgf (1,400 km/h) |
7,845 kgf (1,400 km/h) |
0.99 | 0.98 | 0.93 | 0.86 | 0.81 | 0.58 | |
Survivability and armour
Flares/Chaff
Aircraft countermeasures to distract IR and radar-guided missiles and also AA radar
Crew2 people
Speed of destruction
Structural0 km/h
Gear0 km/h
Examine the survivability of the aircraft. Note how vulnerable the structure is and how secure the pilot is, whether the fuel tanks are armoured, etc. Describe the armour, if there is any, and also mention the vulnerability of other critical aircraft systems.
